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民航运输机减推力起飞技术
Reduced-Thrust Takeoff Technique Applied to Passenger Airplanes
【摘要】 分析了减推力起飞对民航运输机涡轮风扇发动机性能的影响、实施减推力起飞所应具备的必要条件、减推力起飞的性能特点和实施减推力起飞应注意的问题,该研究对正确使用和推广减推力起飞技术,提高航空公司安全管理水平具有重要意义。
【Abstract】 Based on in-depth theoretical research and analysis of the reduced-thrust takeoff performance,this thesis intended to analyze the effect of reduced-thrust takeoff on turbofan engine characteristics,necessity conditions for applying the reduced-thrust takeoff,and cautions related to reduced-thrust takeoff.This research,therefore,aims at helping airlines to apply the reduced-thrust takeoff method properly,to popularize it among pilots gradually and more importantly,to lower cost for airlines and further improve flight safety.
【关键词】 减推力起飞;
涡轮前温度;
发动机使用寿命;
假设温度;
【Key words】 reduced-thrust takeoff; turbine inlet temperature; service life of aero-engine; assumed temperature;
【Key words】 reduced-thrust takeoff; turbine inlet temperature; service life of aero-engine; assumed temperature;
【基金】 中国民用航空总局科研基金资助项目(民航人发[2004]218号,项目17)
- 【文献出处】 飞行力学 ,Flight Dynamics , 编辑部邮箱 ,2009年03期
- 【分类号】V323.19
- 【被引频次】22
- 【下载频次】413